José Nivaldo Hinckel

• Abstract

  In this research project the development of the injector head for a 400 N bipropellant thruster for use in apogee kick engine module is described. The proposal is based on the concept of a compact head where the injector elements and the feed manifold are machined on the face of three plates, one for the distribution of the feed propellants, one for the oxidizer and one for the fuel. The …

  Development of the injector head for 400 n bipropellant thruster for apogee kick engine , AP.PIPE
• 4th European Conference for Aerospace Sciences, AR.EXT

• Abstract

  Recent advances in the development of apogee motors installed in artificial satellites have created an ever greater demand for highly reliable, low weight bi-propellant injectors with reduced energy consumption. Since such components are produced by refined machining processes and electro-erosion, creating a complex network of interconnected cuts and cavities crucial to their functional p…

  Development and manufacture of mono and bi-propellant injectors for low thrust thrusters produced through the process of solid state diffusion soldering, AP.PIPE

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